AU7357198A - Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same - Google Patents

Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same

Info

Publication number
AU7357198A
AU7357198A AU73571/98A AU7357198A AU7357198A AU 7357198 A AU7357198 A AU 7357198A AU 73571/98 A AU73571/98 A AU 73571/98A AU 7357198 A AU7357198 A AU 7357198A AU 7357198 A AU7357198 A AU 7357198A
Authority
AU
Australia
Prior art keywords
inclinations
changing
low energy
computer process
energy method
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU73571/98A
Inventor
Edward A. Belbruno
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of AU7357198A publication Critical patent/AU7357198A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B64G1/2427—Transfer orbits
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/105—Space science
    • B64G1/1064—Space science specifically adapted for interplanetary, solar or interstellar exploration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242—Orbits and trajectories
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244—Spacecraft control systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AU73571/98A 1997-03-25 1998-03-25 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same Abandoned AU7357198A (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US4146597P 1997-03-25 1997-03-25
US60041465 1997-03-25
US4431897P 1997-04-24 1997-04-24
US60044318 1997-04-24
US4824497P 1997-06-02 1997-06-02
US60048244 1997-06-02
PCT/US1998/005784 WO1998042570A2 (en) 1997-03-25 1998-03-25 Method for changing inclinations of orbiting satellites

Publications (1)

Publication Number Publication Date
AU7357198A true AU7357198A (en) 1998-10-20

Family

ID=27365906

Family Applications (1)

Application Number Title Priority Date Filing Date
AU73571/98A Abandoned AU7357198A (en) 1997-03-25 1998-03-25 Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same

Country Status (3)

Country Link
US (1) US6341250B1 (en)
AU (1) AU7357198A (en)
WO (1) WO1998042570A2 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998040675A1 (en) 1997-03-14 1998-09-17 Cove Corporation Plated projectile for use in subsonic ammunition
EP0977686A4 (en) 1997-04-24 2001-05-02 Galaxy Dev Llc Satellite inclination changes using weak stability boundaries
US6149103A (en) * 1998-04-09 2000-11-21 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites havint multiple perilune stages
US6116545A (en) * 1998-04-09 2000-09-12 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites
US7321825B2 (en) * 2003-10-24 2008-01-22 Ford Global Technologies, Llc Method and apparatus for determining vehicle operating conditions and providing a warning or intervention in response to the conditions
US7219858B2 (en) * 2004-07-06 2007-05-22 The Johns Hopkins University Method for deploying multiple spacecraft
US20120119034A1 (en) * 2009-07-02 2012-05-17 Space Systems/Loral, Inc. Deorbiting a Spacecraft from a Highly Inclined Elliptical Orbit
US9284068B2 (en) * 2014-04-08 2016-03-15 The Boeing Company Fast-low energy transfer to Earth-Moon Lagrange point L2
JP6542581B2 (en) * 2015-05-19 2019-07-10 株式会社Ｉｈｉエアロスペース Spacecraft and its orbital plane change method
CN107688725A (en) * 2017-07-26 2018-02-13 西北工业大学 A kind of invariant manifold computational methods based on mixing Lie operator Symplectic Algorithms
CN108860658B (en) * 2018-05-22 2020-08-21 北京理工大学 Plane natural capture method for balanced state double-body asteroid system
CN113071712B (en) * 2021-03-10 2022-07-29 北京空间飞行器总体设计部 Rapid calculation method for monthly transition injection-to-orbit strategy
CN113602534B (en) * 2021-06-26 2023-02-28 山东航天电子技术研究所 On-orbit calibration method for magnitude of micro electric propulsion thrust
CN113960926B (en) * 2021-10-18 2024-04-16 北京理工大学 Self-adaptive adjustment method for pneumatic capturing guidance parameter boundary

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
UST100604I4 (en) 1979-01-29 1981-05-05 Method of placing a spacecraft into final earth orbit or earth escape trajectory
US3532298A (en) 1967-10-31 1970-10-06 Us Navy Method for deploying and stabilizing orbiting structures
US3676581A (en) 1971-02-01 1972-07-11 Us Navy Optical scanning spacecraft system
DE2642061C2 (en) * 1976-09-18 1983-11-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Position control and orbit change method for a three-axis stabilizable satellite, in particular for a geostationary satellite and device for carrying out the method
US4599697A (en) 1982-08-11 1986-07-08 Ford Aerospace & Communications Corporation Digital PWPF three axis spacecraft attitude control
US4618112A (en) 1983-04-15 1986-10-21 Rca Corporation Spacecraft angular momentum stabilization system and method
FR2640933B1 (en) 1988-12-23 1991-04-12 Aerospatiale
FR2647565B1 (en) 1989-04-24 1991-07-26 Alcatel Espace METHOD FOR POSTING A GEOSTATIONARY TELECOMMUNICATIONS SATELLITE
FR2650135B1 (en) * 1989-07-19 1994-05-20 Centre Nal Etudes Spatiales SATELLITE AND METHOD OF ORBITTING BY GRAVITATIONAL ASSISTANCE
US5120008A (en) 1989-07-28 1992-06-09 Kumar Ramohalli Orbital debris processor and method therefor
US5199672A (en) 1990-05-25 1993-04-06 Orbital Sciences Corporation Method and apparatus for deploying a satellite network
US5158249A (en) * 1990-10-12 1992-10-27 Ball Corporation Orbital systems for cislunar travel
US5163640A (en) 1990-12-14 1992-11-17 Hughes Aircraft Company Active spin axis control for spinning space vehicles
US5433726A (en) 1991-04-22 1995-07-18 Trw Inc. Medium-earth-altitude satellite-based cellular telecommunications system
DE4135034C2 (en) 1991-10-23 1995-04-13 Deutsche Forsch Luft Raumfahrt Device for controlling the orbit of at least two co-positioned geostationary satellites
US5421540A (en) 1992-08-26 1995-06-06 Ting; Paul C. Method and apparatus for disposal/recovery of orbiting space debris
US5568904A (en) 1992-08-28 1996-10-29 Space Systems/Loral, Inc. Steered perigee velocity augmentation
US5452869A (en) 1992-12-18 1995-09-26 Hughes Aircraft Company On-board three-axes attitude determination and control system
US5681011A (en) * 1993-08-24 1997-10-28 Orbital Sciences Corporation Method for injecting payloads into orbit
US5595360A (en) * 1994-03-25 1997-01-21 Hughes Aircraft Company Optimal transfer orbit trajectory using electric propulsion

Also Published As

Publication number Publication date
WO1998042570A3 (en) 1998-12-30
US6341250B1 (en) 2002-01-22
WO1998042570A2 (en) 1998-10-01

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